Influence of γ' precipitate on deformation and fracture during creep in PM nickel-based superalloy

FGH96 is a powder metallurgy nickel based superally used for turbine disk of aero-engines. In the present study FGH96 alloy with four different γ' precipitate microstructures were produced via solution heat-treatment with different cooling rates, and the maximum cooling rate reached 400°C/min which was a super cooling rate for Nickel-based superalloy. The creep tests were conducted for PM FGH96 alloy under the testing condition of 704°C and 690 MPa. The relationship between the creep properties and the distribution of γ' precipitate was established. The creep mechanism was analyzed by using TEM and ACTEM, and the dislocation movement was studied at the atomic scale. The creep strain rate was calculated through a physically based crystal slip model established based on crystal plasticity. The calculated results were consistent with the test ones, illustrating the validity of the model. The fracture mechanism was also investigated, and the results showed that the creep cracks generated on the surface due to the oxidation. It was observed that the cracks propagated in different ways depending on the different average diameters of γ' precipitate. With the decrease of the average γ' precipitate size,the critical shearing stress increased and the resistance of the dislocation slipping increased. The fracture mechanism for the primary stage transformed from intragranular to intergranular due to the change of dislocation slipping.     

镍基单晶高温合金蠕变机制研究进展

 叶片在服役过程中主要承受〈001〉轴向的离心载荷，由离心应力导致的蠕变损伤是叶片的主要失效机制之一。基于单晶叶片的典型服役条件，总结了国内外关于高温低应力和中温高应力蠕变变形损伤机制的研究现状，指出深入开展含典型缺陷单晶高温合金蠕变行为、氧化和热腐蚀对单晶合金蠕变-疲劳变形损伤机制影响研究十分必要。     

热等静压技术在镍基单晶高温合金中的应用研究进展

 通过总结目前热等静压对镍基单晶高温的应用研究进展，阐释了热等静压对镍基单晶高温合金中的疏松等孔洞类缺陷的消除作用，分析了孔洞的愈合机理，并分别展示了应用热等静压后合金的拉伸、持久、疲劳等力学性能变化情况，同时介绍了热等静压对已服役制件组织力学性能恢复处理的研究进展、计算模拟在指导热等静压工艺研究中的作用，展望了中国热等静压技术的未来发展。     

镍基催化剂对乙烷氧化脱氢制乙烯性能的研究

用均匀沉淀法制备了片状复合氧化镍NiMO(M=Li,Sr,Y,Fe,La)催化剂,并研究了其对乙烷氧化脱氢制乙烯的催化性能.采用X射线衍射(XRD)、扫描电子显微镜(SEM)、程序升温还原(H2-TPR)和程序升温脱附(O2-TPD)等方法对镍基催化剂进行了表征.X射线衍射和扫描电子显微镜检测结果表明:助剂的加入对催化剂的形貌影响不大,仍为片状结构;平均粒径为5~10 nm.程序升温还原和脱附表征结果表明:助剂Li,Sr并未进入NiO晶格;而助剂Y,Fe,La与Ni之间具有相互作用,因而影响催化剂的理化性质和催化活性.其中,Fe掺杂的片状氧化镍催化剂对乙烯的选择性和收率均有所改善,340℃时NiFeO催化剂上的乙烯收率可达18.2%.     

工艺参数对低铝钛GH600合金显微组织及析出相的影响

利用Gleeble3800热模拟实验机,对低铝钛GH600合金进行热压缩实验;利用金相显微镜研究工艺参数对显微组织演变规律的影响;利用透射电镜及能谱观察分析析出相、位错等微观结构。结果表明:提高变形量可以得到细晶组织,改善合金的使用性能,并且在大变形量下,动态再结晶容易进行,软化效果得到提高,在一定程度上改善合金的加工性能。当变形温度升高时,再结晶比例得到很大的提高,合金动态再结晶体积分数增大,位错密度降低,使加工容易进行。但当变形温度过高时,再结晶组织会出现粗化现象。低铝钛GH600合金的优选热加工工艺参数为:温度1 100~1 150℃,变形量60%。在这种工艺条件下,合金中的再结晶程度最高,再结晶晶粒没有出现粗化现象,并且析出相的成分、尺寸也为理想状态。     

NiCoCrAlYTa粘结层与镍基高温合金基体的界面高温互扩散行为

采用真空等离子体喷涂技术(vacuum plasma spraying, VPS)在镍基高温合金GH3128基体表面沉积NiCoCrAlYTa粘结层,并在1 100 ℃进行不同时间的热处理。采用扫描电子显微镜（scanning electron microscopy,SEM）、能谱仪（energy dispersive spectrometer,EDS）等分析NiCoCrAlYTa粘结层与GH3128高温合金界面元素的互扩散行为。结果表明,在热处理过程中,互扩散区(interdiffusion zone,IDZ)和二次反应区(secondary reaction zone,SRZ)的厚度随着热处理时间延长而增大,且在SRZ中明显观察到拓扑密堆(topological close-packed,TCP)相晶粒的生长。Al、Ta、Co元素由NiCoCrAlYTa粘结层向GH3128高温合金扩散,Ni、W、Mo元素由GH3128高温合金向NiCoCrAlYTa粘结层扩散。依据EDS检测的粘结层/基体界面处元素成分,计算出上述元素在界面处的扩散系数,掌握了各元素在高温热处理过程中的扩散速率,揭示了VPS制备的NiCoCrAlYTa粘结层与GH3128高温合金界面处元素在高温下的互扩散规律。     

一种单晶高温合金中g?相的析出行为

研究了固溶冷却速度和时效时间对一种镍基单晶高温合金中γ′相的析出的影响。合金经1 250℃固溶处理4 h,从炉中快速取出,分别进行空冷、油冷和水冷,以考察冷却速度对γ′相析出的影响。随后对固溶处理后试样进行时效处理,以考察时效时间和固溶冷却速度对γ′相长大的影响。结果表明,合金在固溶处理后,γ′相尺寸随固溶冷却速率的升高而下降。在时效处理时,γ′相尺寸的增大率随固溶冷却速度的增大而减小;随着时效时间的增加,γ′相的尺寸增加。     

FGH95镍基合金组织结构对持久性能的影响

通过对不同温度热等静压FGH95合金进行完全热处理、组织形貌观察、XRD谱线分析及持久性能测试,研究FGH95合金组织结构对持久性能的影响。结果表明:随着HIP温度升高,分布在原始颗粒边界处的粗大γ′相数量和尺寸逐渐减小,当HIP温度提高至1 180℃,晶粒明显长大。热等静压合金经完全热处理后,粒状碳化物沿晶界和晶内不连续分布,且细小γ′相在基体中弥散析出。经X线衍射分析,随热等静压温度升高,γ和γ′两相晶格常数略有增加,但错配度逐渐减小;在650℃,1 034 MPa条件下,由于1 120℃HIP合金完全热处理后具有较高的晶格错配度,致使合金具有较长持久寿命;合金在蠕变期间的变形特征是位错滑移,位错绕过或剪切γ′相。     

Microstructure and heat treatment for Ni3Al-based single crystal alloy with different crystal orientations

Ni₃Al-based single crystal alloy IC6SX with different crystal orientations were prepared by seed crystal method. The microstructure and heat treatment of the alloy were investigated. The results showed that the microstructure of the alloy was in dendrite structure, and the crystal orientation had significant effect on the dendrite morphology of this alloy. The precipitated phases of (MoNi)₆C and NiMo appeared in the microstructure of the three alloys with different crystal orientations during solidification process. Compared with other two alloys, the volume fractions of precipitated phases of both (MoNi)₆C and NiMo was the most in the alloy with [111] orientation and the least in the alloy with [001] orientation. The solidus and liquidus temperatures of the alloy IC6SX tested by differential scanning calorimetry (DSC) were 1356 °C and 1387 °C, respectively. Meanwhile, the effect of different solution temperatures on the microstructure of the alloy with different orientations was studied. The results showed that the precipitated phases of (MoNi)₆C and NiMo were eliminated with the solid solution treatment under the condition of 1300 °C/10 h. However, the incipient melting of the alloys occurred due to the dissolution of low melting point phases. As the temperature dropped to 1280 °C, the area of incipient melting in the alloy with different orientations decreased gradually. However, there was no incipient melting appearing in the three alloys with different orientations when the solution treatment temperature dropped to 1260 °C.     

助剂改性镍铈负载橄榄石焦油裂解催化剂的研究

以镍为活性组分,二氧化铈为助催化剂,橄榄石为载体研究了橄榄石负载镍催化剂的催化性能,实验还考察了不同助剂(Cu,Fe,Mg)的添加对催化剂活性的影响,结果表明,Cu,Fe,Mg都能提高Ce-Ni/Olivine催化剂焦油裂解活性和燃气质量,其中Cu效果最佳.